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At a glance
Measured figures
Empty; A-10C · Empty weight
Single sourceGross; A-10C · Anti-armor mission
Single sourceGross; A-10C · Close air support (CAS)
Single sourceGross; A-10C · mission
Single sourceMaximum take-off; A-10C · Max takeoff weight
Single source24,959 lb (11,321 kg)[source]
30,384 lb (13,782 kg) Close air support (CAS) mission: 47,094 lb (21,361 kg) Anti-armor mission: 42,071 lb (19,083 kg)[source]
46,000 lb (20,865 kg)[source]
Cruise; A-10C · Cruise speed
Single sourceMaximum; A-10C · at sea level, clean
Single source381 kn (439 mph, 706 km/h) at sea level, clean[source]
300 kn (340 mph, 560 km/h)[source]
Maximum; F-15E · at low altitude
Single sourceMaximum; F-15E · Mach 2.5 at high altitude Mach 1.2
Single sourceMach 2.5, 1,650 mph (2,655 km/h) at high altitude Mach 1.2, 800 kn (921 mph; 1,482 km/h) at low altitude[source]
Ferry; A-10C · with 50 knots (58 mph; 26 m/s) headwinds, 20 minutes reserve
Single source2,240 nmi (2,580 mi, 4,150 km) with 50 knots (58 mph; 26 m/s) headwinds, 20 minutes reserve[source]
Ferry; F-15E · with conformal fuel tanks and three external fuel tanks
Single source2,100 nmi (2,400 mi, 3,900 km) with conformal fuel tanks and three external fuel tanks[source]
A-10C · and 10 minutes of combat Anti-armor mission with sea-level penetration and exit, 30 min combat
Single sourceA-10C · CAS mission representing a 1 hour 53 minute of loiter time at 5,000 ft (1,500 m)
Single sourceA-10C · Combat range
Single source250 nmi (288 mi, 463 km) CAS mission: 250 nmi (290 mi; 460 km) representing a 1 hour 53 minute of loiter time at 5,000 ft (1,500 m), and 10 minutes of combat Anti-armor mission: 252 nmi (290 mi; 467 km) with sea-level penetration and exit, 30 min combat[source]
F-15E · air interdiction
Single source687 nmi (791 mi, 1,272 km) air interdiction[source]
A-10C · 2 × General Electric TF34 -GE-100A turbofans thrust each
Single source2 × General Electric TF34 -GE-100A turbofans , 9,065 lbf (40.32 kN) thrust each[source]
F-15E · ); 29,160 lb (
Single sourceF-15E · 2 × Pratt & Whitney F100-PW-220 afterburning turbofan thrust each dry
Single sourceF-15E · ) with afterburner each
Single sourceF-15E · with afterburner ( or 2 × F100-PW-229 , thrust: 17,800 lb dry (
Single source2 × Pratt & Whitney F100-PW-220 afterburning turbofan , 14,590 lbf (64.9 kN) thrust each dry, 23,770 lbf (105.7 kN) with afterburner ( or 2 × F100-PW-229 , thrust: 17,800 lb dry (79 kN); 29,160 lb (129.7 kN) with afterburner each)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Fairchild Republic A-10 Thunderbolt II | McDonnell Douglas F-15E Strike Eagle |
|---|---|---|
| Type | Close air support attack aircraft[source] | Multirole strike fighter[source] |
| National origin | United States[source] | United States[source] |
| Manufacturer | Fairchild Republic[source] | McDonnell Douglas (1985–1997) Boeing Defense, Space & Security (1997–2017)[source] |
| Status | In service[source] | In service[source] |
| Primary user | United States Air Force[source] | — |
| Number built | 716[source] | 435 (F-15E/I/S/K/SG)[source] |
| Manufactured | 1972–1984[source] | 1985–2017[source] |
| Introduction date | October 1977[source] | 1988 30 September 1989 ( IOC )[source] |
| First flight | 10 May 1972 ( 1972-05-10 )[source] | 11 December 1986 ( 1986-12-11 )[source] |
| Fuel capacity | 11,000 lb (4,990 kg) internal[source] | 12,915 lb (5,858 kg) internal, 22,267 lb (10,100 kg) with CFTs, 34,162 lb (15,496 kg) with CFTs and 3× 600-gallon (2,270 L) external fuel tanks[source] |
| Guns | 1× 30 mm (1.18 in) GAU-8/A Avenger rotary cannon with 1,174 rounds[source] | 1× 20 mm (0.787 in) M61A1 Vulcan 6-barreled rotary cannon , 500 rounds of either M-56 or PGU-28 ammunition[source] |
| Hardpoints | 11 (8× under-wing and 3× under-fuselage pylon stations) with a capacity of 16,000 lb (7,260 kg), with provisions to carry combinations of: Rockets: 4× LAU-61/LAU-68 rocket pods (each with 19×/7× Hydra 70 mm/ APKWS rockets, respectively) 6× LAU-131 rocket pods (each with 7× Hydra 70 rockets) Missiles: 4× AIM-9 Sidewinder air-to-air missiles for self-defense 6× AGM-65 Maverick air-to-ground missiles Bombs: Mark 80 series of unguided 'iron' bombs or Mk 77 incendiary bombs or BLU-1, BLU-27/B, CBU-20 Rockeye II, BL755 and CBU-52/58/71/87/89/97 cluster bombs or Paveway series of Laser-guided bombs or Joint Direct Attack Munition (JDAM) (A-10C) or Wind Corrected Munitions Dispenser Other: SUU-42A/A Flares/infrared decoys and chaff dispenser pod or 2× 600 US gal (2,300 L) Sargent Fletcher drop tanks for increased range/loiter time.[source] | 4 wing pylons, fuselage pylons, bomb racks on CFTs with a capacity of 23,000 lb (10,400 kg) of external fuel and ordnance[source] |
| Airfoil | NACA 6716 root, NACA 6713 tip[source] | root: NACA 64A006.6 ; tip: NACA 64A203[source] |
| Close air support (CAS) mission | 47,094 lb (21,361 kg)[source] | — |
| Anti-armor mission | 42,071 lb (19,083 kg)[source] | — |
| Stall speed | 120 kn (138 mph, 220 km/h) at 30,000 lb (14,000 kg)[source] | — |
| Never exceed speed | 450 kn (518 mph, 833 km/h) at 5,000 ft (1,500 m) with 18 Mark 82 bombs[source] | — |
| CAS mission | 250 nmi (290 mi; 460 km) representing a 1 hour 53 minute of loiter time at 5,000 ft (1,500 m), and 10 minutes of combat[source] | — |
| Wing loading | 99 lb/sq ft (482 kg/m 2 )[source] | — |
| Thrust/weight | 0.47[source] | 0.93[source] |
| Rockets | 4× LAU-61/LAU-68 rocket pods (each with 19×/7× Hydra 70 mm/ APKWS rockets, respectively) 6× LAU-131 rocket pods (each with 7× Hydra 70 rockets)[source] | — |
| Missiles | 4× AIM-9 Sidewinder air-to-air missiles for self-defense 6× AGM-65 Maverick air-to-ground missiles[source] | Air-to-air missiles : 4× AIM-7 Sparrow 4× AIM-9 Sidewinder or IRIS-T (S variant of the Saudi Air Force ) 8× AIM-120 AMRAAM Air-to-surface missiles : 6× AGM-65 Maverick 2× AGM-84 Harpoon 2× AGM-84H/K SLAM-ER 2x AGM-130 AGM-154 JSOW AGM-158 JASSM Joint Strike Missile (to be integrated) Taurus KEPD 350 (integrated on South Korean Air Force F-15Ks)[source] |
| Bombs | Mark 80 series of unguided 'iron' bombs or Mk 77 incendiary bombs or BLU-1, BLU-27/B, CBU-20 Rockeye II, BL755 and CBU-52/58/71/87/89/97 cluster bombs or Paveway series of Laser-guided bombs or Joint Direct Attack Munition (JDAM) (A-10C) or Wind Corrected Munitions Dispenser[source] | Mark 82 bomb Mark 84 bomb GBU-15 GBU-10 Paveway II GBU-12 Paveway II GBU-24 Paveway III GBU-27 Paveway III GBU-28 (Bunker buster) GBU-31 or GBU-38 {8 GBU-31s or 16 GBU-38s} (JDAM) GBU-54 Laser JDAM (LJDAM) GBU-39 Small Diameter Bomb (SDB) B61 nuclear bomb CBU-87 or CBU-103 (CEM) CBU-89 or CBU-104 (GATOR) KGGB (integrated on South Korean Air Force F-15Ks) CBU-97 or CBU-105 (SFW) CBU-107 Passive Attack Weapon BLU-107 Durandal[source] |
| Other | SUU-42A/A Flares/infrared decoys and chaff dispenser pod or 2× 600 US gal (2,300 L) Sargent Fletcher drop tanks for increased range/loiter time.[source] | — |
| Targeting pods | AN/AAQ-28(V)4 LITENING or AN/AAQ-33(V)1/2 Sniper[source] | AN/AAQ-14 LANTIRN or Lockheed Martin Sniper XR or AN/AAQ-28(V) Litening[source] |
| Countermeasures | AN/ALQ-131 or AN/ALQ-184(V)-11/12 ECM pods[source] | Northrop Grumman Electronic Systems AN/ALQ-131 electronic countermeasures pod Hazeltine AN/APX-76 or Raytheon AN/APX-119 Identify Friend/Foe (IFF) interrogator Magnavox AN/ALQ-128 Electronic Warfare Warning Set (EWWS) – part of Tactical Electronic Warfare Systems (TEWS) Loral AN/ALR-56 Radar warning receivers (RWR) – part of TEWS Northrop Grumman Electronic Systems ALQ-135 Internal Countermeasures System (ICS) – part of TEWS Marconi AN/ALE-45 Chaff / Flares dispenser system – part of TEWS BAE Systems AN/ALQ-250 Eagle Passive Active Warning Survivability System (EPAWSS) - combined electronic warfare / electronic countermeasures system[source] |
| Primary users | — | United States Air Force Royal Saudi Air Force Israeli Air Force Republic of Korea Air Force For other users, see Operators[source] |
| Developed from | — | McDonnell Douglas F-15 Eagle[source] |
| Variant | — | Boeing F-15SE Silent Eagle[source] |
| Developed into | — | Boeing F-15EX Eagle II[source] |
| g limits | — | + 9[source] |
| Others | — | up to 3× 600 US gallons (2,300 L ) external drop tanks for ferry flight or extended range/loitering time 3 x 7-round (21) APKWS under each wing[source] |
| Radar | — | Raytheon AN/APG-70 or AN/APG-82 AN/ASQ-236 Radar Pod[source] |